Promising solutions for fully reusable two-stage-to-orbit configurations (original) (raw)

Assessment of multiple mission reusable launch vehicles

Aaron Koch

Journal of Space Safety Engineering, 2019

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First stage design variations of partially reusable launch vehicles

Volker Schmid

2001

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High-Payoff Space Transportation Design Approach with a Technology Integration Strategy

Russel Rhodes

47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2011

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Technology Requirements for Affordable Single-Stage Rocket Launch Vehicles

Douglas Stanley

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A Study of ARTS: A Dual-Fuel Reusable Launch Vehicle (RLV) with Launch Assist

John Olds

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2003

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An Integrated Design and Intelligent Optimization Framework for Forebody-Inlet Configuration of Booster Stage and Mass-Model of Two-Stage-to-Orbit Space Plane

Ali Sarosh

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Rocket-powered single-stage-to-orbit vehicles for safe economical access to low Earth orbit

Last Renegade

Acta Astronautica, 1992

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Basic Research and Technologies for Two-Stage-to-Orbit Vehicles

Michal Kapusňák

Basic Research and Technologies for Two-Stage-to-Orbit Vehicles, 2005

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The Importance of Detailed Component Simulations in the Feedsystem Development for a Two-Stage-to-Orbit Reusable Launch Vehicle

Frank Chandler

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005

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RETALT: Development of Key Flight Dynamics and GNC Technologies for Reusable Launchers

Giuseppe Guidotti

Zenodo (CERN European Organization for Nuclear Research), 2022

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Life Cycle Systems Engineering Approach to NASA's 2nd Generation Reusable Launch Vehicle

Dale Thomas

2002

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The Stellar-J: A Partially Reusable Horizontal Take-Off Launch Vehicle For Small Satellite Missions

wes kelly

2008

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The Stellar-J: A Partially Reusable Horizontal Take-Off Launch System Designed for Small Satellite and Low Startup Cost

wes kelly

2009

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Future reusable launch vehicles in europe: the FLTP (Future Launchers Technologies Programme)

Christophe BONNAL

Acta Astronautica, 2000

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Design options for advanced manned launch systems (AMLS)

Alan Wilhite

1990

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Modern Trends in the Development of Reusable Aerospace System

Yuri Khlopkov, Zay Yar Myo Myint

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Cost Comparison of Expendable, Hybrid, and Reusable Launch Vehicles

John Livingston

Space 2006, 2006

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Deriving an Acceptable Level of Reusable Launch Vehicle Flightworthiness

Rene Rey

AIP Conference Proceedings, 2000

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Multidisciplinary design of a rocket-based combined-cycle SSTO launch vehicle using Taguchi Methods

John Olds

AIAA paper, 1993

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A conceptual design for a single-stage-to-orbit Space Station service vehicle

John Olds

26th Aerospace Sciences Meeting, 1988

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A Performance Analysis of a Rocket Based Combined Cycle (RBCC) Propulsion System for Single-Stage-To-Orbit Vehicle Applications

Nehemiah Williams

2010

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A Comparison of Horizontal Takeoff RLVs for Next Generation Space Transportation

Last Renegade

AIAA Paper, 2003

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Paper Session I-A - Space Shuttle to Reusable Launch Vehicle

Russel Rhodes

1995

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Optimization of Liquid Rocket propulsion system for Reusable Orbital Transfer Vehicle

Igor Borovik

IOP Conference Series: Materials Science and Engineering, 2019

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A Technology Pathway for Airbreathing, Combined-Cycle, Horizontal Space Launch Through SR-71 Based Trajectory Modeling

Kurt Kloesel

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2011

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Prediction of the Aerodynamic Performance of Re-Usable Single Stage to Orbit Vehicles

Abdul Jabbar Ahmad

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First Stage of a Highly Reliable Reusable Launch System

Kurt Kloesel

AIAA SPACE 2009 Conference & Exposition, 2009

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Design options for advanced manned launch systems

Alan Wilhite

Journal of Spacecraft and Rockets, 1995

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Structural and loads analysis of a two-stage fully reusable AdvancedManned Launch System

Douglas Stanley

4th Symposium on Multidisciplinary Analysis and Optimization, 1992

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D4OPS: Design for Operations of Future Reusable Launch Systems

John Olds, Edgar Zapata

International Astronautical Congress, 2004

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Dual-fuel propulsion in single-stage Advanced Manned Launch System Vehicle

Douglas Stanley

Journal of Spacecraft and Rockets, 1995

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Multi-Disciplinary System Design Optimization of a Launch Vehicle Upper-Stage

Journal of Aerospace Technology and Management, mostafa zakeri

Journal of Aerospace Technology and Management, 2017

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Multi-Disciplinary Analysis for Future Launch Systems Using NASA's Advanced Engineering Environment (AEE)

james reuther

16th AIAA Computational Fluid Dynamics Conference, 2003

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Application of a new economic analysis tool to a two-stage-to-orbit RBCC launch vehicle design

John Olds

6th Symposium on Multidisciplinary Analysis and Optimization, 1996

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